WASET
	@article{(Open Science Index):https://publications.waset.org/pdf/16467,
	  title     = {Preliminary Development of a Hydrogen Peroxide Thruster},
	  author    = {Y. A. Chan and  H. J. Liu and  K. C. Tseng and  T. C. Kuo},
	  country	= {},
	  institution	= {},
	  abstract     = {Green propellants used for satellite-level propulsion
system become attractive in recent years because the non-toxicity and
lower requirements of safety protection. One of the green propellants,
high-concentration hydrogen peroxide H2O2 solution (≥70% w/w,
weight concentration percentage), often known as high-test peroxide
(HTP), is considered because it is ITAR-free, easy to manufacture and
the operating temperature is lower than traditional monopropellant
propulsion. To establish satellite propulsion technology, the National
Space Organization (NSPO) in Taiwan has initialized a long-term
cooperation project with the National Cheng Kung University to
develop compatible tank and thruster. An experimental propulsion
payload has been allocated for the future self-reliant satellite to
perform orbit transfer and maintenance operations. In the present
research, an 1-Newton thruster prototype is designed and the thrusting
force is measured by a pendulum-type platform. The preliminary
hot-firing test at ambient environment showed the generated thrust and
the specific impulse are about 0.7 Newton and 102 seconds,
respectively.
},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {7},
	  number    = {7},
	  year      = {2013},
	  pages     = {1546 - 1553},
	  ee        = {https://publications.waset.org/pdf/16467},
	  url   	= {https://publications.waset.org/vol/79},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 79, 2013},
	}